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Applied Mathematics and Nonlinear Sciences
Band 3 (2018): Heft 1 (June 2018)
Uneingeschränkter Zugang
The Triaxiality Role in the Spin-Orbit Dynamics of a Rigid Body
A. Cantero
A. Cantero
,
F. Crespo
F. Crespo
und
S. Ferrer
S. Ferrer
| 03. Okt. 2018
Applied Mathematics and Nonlinear Sciences
Band 3 (2018): Heft 1 (June 2018)
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Online veröffentlicht:
03. Okt. 2018
Seitenbereich:
187 - 208
Eingereicht:
06. Feb. 2018
Akzeptiert:
21. Mai 2018
DOI:
https://doi.org/10.21042/AMNS.2018.1.00015
Schlüsselwörter
Rotational and orbital dynamics
,
gravity-gradient
,
intermediary
,
relative equilibria
© 2018 A. Cantero et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.
Fig. 1
Geometry of the variables (r, φ, ψ, θ, δ, ν, R, Φ, Ψ, Θ, Δ, N). The variable r and the angles are explicitly given in the figure, while the associated momenta are included implicitly through the inclinations of the planes. The conjugate variable R remains unrepresented because of its pure dynamical sense.
Fig. 2
Columns from left to right we have: (i)ρ = 0, A1 = 9.80 · 1020, A2 = 9.8 · 1020, A3 = 1.07 · 1021. (ii)ρ = 0.0005, A1 = 1.17 · 1021, A2 = 1.23 · 1021, A3 = 1.39 · 1021. Abscissas are orbital periods and D[x] = xFull–xIntermediary. The orbital period is 10.8 hours and r is expressed in Km, which initially is set to 1.560 Km.
Fig. 3
Columns from left to right we have: (i)ρ = 0, A1 = 9.80 · 1020, A2 = 9.8 · 1020, A3 = 1.07 · 1021. (ii)ρ = 0.15, A1 = 1.17 · 1021, A2 = 1.23 · 1021, A3 = 1.39 · 1021. (iii)ρ = 0.35, A1 = 1.06 · 1021, A2 = 1.18 · 1021, A3 = 1.28 · 1021. Abscissas are orbital periods and D[x] = xFull–xIntermediary. The orbital period is 10.8 hours and r is expressed in Km, which initially is set to 1.560 Km.
Fig. 4
Left column e = 0.1 and right column e = 0.5.Abscissas are orbital periods and D[x] = xFull–xIntermediary. The orbital period is 10.8 hours and r is expressed in Km, which initially is set to 1.560 Km.
Fig. 5
Left column (H = 1000Km, T = 22.8h) and right column (H = 2000Km, T = 10.8h), where T is the orbital period expressed in hours. Abscissas are orbital periods and D[x] = xFull–xIntermediary
Fig. 6
(Left) triaxiality region with τ1 = 0.35 and τ2 = 0.9. (Right) Curves cσ1 and cσ2 restricted to interval [0, 1] for ζ = 0.7.
Fig. 7
Parameters: ζ = 0.2, τ1 = 0.3, τ2 = 0.75.
Fig. 8
Parameters: ζ = 0.2, τ1 = 0.6, τ2 = 0.75.
Fig. 9
Special relative equilibria of the body-perpendicular type with ν = ±nπ.
Fig. 10
Special relative equilibria of the body-inclined type.
Fig. 11
Spherical triangles involved in the problem. α is the angle between the two nodes of the orbital plane. (a) Triangle formed by the orbital angular momentum plane, the total angular momentum plane and the reference plane. (b) Triangle formed by the rotational angular momentum plane, the total angular momentum plane and the reference plane.
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